How to Calculate Eccentricity w.r.t axis XX given Total Stress where Load doesn't lie on Plane?
Eccentricity w.r.t axis XX given Total Stress where Load doesn't lie on Plane calculator uses Eccentricity with respect to Principal Axis XX = ((Total Stress-(Axial Load/Cross-Sectional Area)-((Eccentricity with respect to Principal Axis YY*Axial Load*Distance from YY to Outermost Fiber)/(Moment of Inertia about Y-Axis)))*Moment of Inertia about X-Axis)/(Axial Load*Distance from XX to Outermost Fiber) to calculate the Eccentricity with respect to Principal Axis XX, The Eccentricity w.r.t axis XX given Total Stress where Load doesn't lie on Plane formula is defined as the eccentricity of a conic section is a non-negative real number that uniquely characterizes its shape. Eccentricity with respect to Principal Axis XX is denoted by ey symbol.
How to calculate Eccentricity w.r.t axis XX given Total Stress where Load doesn't lie on Plane using this online calculator? To use this online calculator for Eccentricity w.r.t axis XX given Total Stress where Load doesn't lie on Plane, enter Total Stress (σtotal), Axial Load (P), Cross-Sectional Area (Acs), Eccentricity with respect to Principal Axis YY (ex), Distance from YY to Outermost Fiber (cx), Moment of Inertia about Y-Axis (Iy), Moment of Inertia about X-Axis (Ix) & Distance from XX to Outermost Fiber (cy) and hit the calculate button. Here is how the Eccentricity w.r.t axis XX given Total Stress where Load doesn't lie on Plane calculation can be explained with given input values -> 15.76877 = ((14.8-(9990/13)-((4*9990*0.015)/(50)))*51)/(9990*0.014).